US4799231A - Laser gas orifice injection system - Google Patents
Laser gas orifice injection system Download PDFInfo
- Publication number
- US4799231A US4799231A US07/101,130 US10113087A US4799231A US 4799231 A US4799231 A US 4799231A US 10113087 A US10113087 A US 10113087A US 4799231 A US4799231 A US 4799231A
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- United States
- Prior art keywords
- orifice
- tube
- electrode
- longitudinal axis
- gas
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/03—Constructional details of gas laser discharge tubes
- H01S3/038—Electrodes, e.g. special shape, configuration or composition
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/03—Constructional details of gas laser discharge tubes
- H01S3/036—Means for obtaining or maintaining the desired gas pressure within the tube, e.g. by gettering, replenishing; Means for circulating the gas, e.g. for equalising the pressure within the tube
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/05—Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
- H01S3/06—Construction or shape of active medium
- H01S3/07—Construction or shape of active medium consisting of a plurality of parts, e.g. segments
- H01S3/073—Gas lasers comprising separate discharge sections in one cavity, e.g. hybrid lasers
- H01S3/076—Folded-path lasers
Definitions
- the present invention relates to an improved gas laser, and/or components thereof. More particularly, the present invention relates to an improved structure for introducing gas into the optical resonator of a gas laser.
- a laser has many components. Because a laser is a precision instrument, many of these components must be of high precision.
- One such component is the optical resonator structure.
- the optical resonator structure has a cavity in which the active lasing medium is excited to produce the beam of coherent radiation.
- a first highly polished mirror At one end of the optical resonator cavity is a first highly polished mirror, which is nearly one hundred percent (100%) reflective; a second highly polished mirror is at the other end, which is less reflective than the first mirror and permits some of the radiation to be transmitted as useful output therethrough.
- a gaseous lasing medium flows in the optical resonator generally parallel to the optical resonator's longitudinal axis.
- One or more anode-cathode pairs each introduce an electric field in the flowing gas to create a volume of plasma, sometimes referred to as the "discharge region" or “discharge volume,” in the optical resonator.
- the contents of the optical resonator are heated by the electric field.
- the purpose for circulating gas within the resonator is to remove heated gas and substitute cooler gas therefor.
- the removed gas (which may be a pure gas or a mixture of gasses) is typically cooled in a heat exchanger and recycled for use in the resonator.
- the discharge region is not limited to an undesirably small portion of the resonator cavity (such as, for example, within a small distance from the longitudinal axis of the resonator tube). If the discharge volume moves irregularly, the laser's coherent radiation output will vary accordingly. If the discharge volume is too small, the maximum output of the laser is accordingly limited.
- the inventive laser resonator system includes an optical resonator whose side wall has an orifice through which gas may enter the resonator's interior, and may subsequently flow along the resonator's longitudinal axis.
- An elongated electrode (which preferably is an anode, but may optionally be a cathode) is positioned at the orifice in electrical communication with the entering gas so that the projection of the electrode's tip on the plane of the orifice does not coincide with the orifice's center.
- the electrode's longitudinal axis is aligned generally perpendicular to the plane of the orifice.
- two such electrode-orifice pairs are separated by a small distance along the resonator's axis, and the two orifices are positioned on opposite sides of the resonator, so that the orifices are separated by an azimuthal angle substantially equal to 180° with respect to the resonator's axis.
- FIG. 1 is a side view of a resonator structure of a gas laser that embodies the present invention.
- FIG. 2 is a cross-sectional view of the FIG. 1 laser, taken along the line 2--2 of FIG. 1.
- FIG. 3 is a cross-sectional view of the FIG. 1 laser, taken along the line 3--3 of FIG. 1.
- FIG. 4 is a cross-sectional view (in a horizontal plane intersecting the axis of the gas discharge tube of FIG. 1) of a preferred type of gas injection element that may be used in the FIG. 1 system.
- FIG. 5 is a cross-sectional view of the left half of the FIG. 4 apparatus, taken along line 5--5 of FIG. 4.
- FIG. 6 is a cross-sectional view of a portion of the inventive system showing a preferred orientation of an electrode of the system relative to a gas inlet orifice of the system.
- FIG. 1 is a side view of laser resonator structure 24. Although for specificity, the discussion set forth hereinafter will sometimes identify structure 24 as a portion of an axial flow CO 2 type of laser, it should be apparent that the invention is not so limited. It is contemplated that the invention can be used in any type of laser having an axially flowing gaseous lasing medium.
- gas is passed from within support tube 40 into discharge tube 26.
- the discharge tube will sometimes be referred to herein as the "laser resonator tube” or the “optical resonator tube” or simply as the “resonator tube”.
- laser resonator tube the lasing action of the gas is produced, generating a beam of coherent radiation.
- branch pipes 80 the gas flows from resonator tube 26 through branch pipes 80 to exhaust tube 27.
- Support tube 40 aligns and supports the optical resonator structure 24 with a first mirror 42 positioned on a first end bracket 41 at one end of the support tube 40 and a second mirror 44 positioned on a second end bracket 43 at the other end of the support tube 40.
- the support tube 40 is attached to each end bracket 41 and 43, and is positioned substantially parallel to the discharge tube 26.
- Gas from the support tube 40 is passed to the discharge tube 26 substantially near the ends of the support tube 40 and of the discharge tube 26 in a radial direction from the support tube 40 to the discharge tube 26.
- Once the gas is introduced into the discharge tube 26, it flows axially away from the ends of the discharge tube 26. Away from the ends of the discharge tube 26, the gas from the discharge tube 26 is passed through branch pipes 80 to the exhaust tube 27.
- discharge tubes 26 there are two discharge tubes 26 in communication with the support tube 40 and the exhaust tube 27. Any number of discharge tubes 26 can be placed parallel to the support tube 40 and in communication therewith. However, preferably, the discharge tubes 26 are positioned axially spaced from one another by approximately 90 degrees. Also preferably for structural support, the support tube 40 should be positioned substantially near the center of the optical resonator structure 24 to achieve the greatest stability and alignment.
- gas within the support tube 40 is maintained at a substantially constant temperature. Furthermore, preferably, the temperature of the gas within the support tube 40 is maintained above the ambient temperature.
- the stability of the optical resonator structure 24 and the alignment of the first and second mirrors 42 and 44 and the folding mirrors 5 are less likely to be affected by temperature variations in the ambient or in the structure 24 caused by the excitation of the gas in the discharge tube 26.
- a plurality of anodes 65 and cathodes 64 are mounted along discharge tube 26 in electrical communication with the gas flowing therein.
- the anodes are mounted in gas inlet structures 62 to be described in greater detail below.
- the anodes 65 and cathodes 64 are preferably spaced approximately 11.25 inches apart.
- the sections of discharge tube 26 between each structure 62 and each outlet structure 81 are preferably 14 inches in length, and there are either four, eight, or sixteen such sections per laser.
- Electrical lines 70 connect the anodes to the positive ground terminal of a DC power source (not shown) and electrical lines 71 connect the cathodes to the negative high voltage terminal of a DC power source (not shown).
- the outer diameter of the discharge tube is preferably 20 mm. with an inner diameter of 18 mm.
- the anodes 65 are preferably positioned substantially near the ends of the discharge tube 26 and near the gas inlets from the support tube 40.
- the cathodes 64 are preferably positioned away from the ends of the discharge tube 26 near the gas exhaust from the discharge tube 26 to the exhaust tube 27. In the event more than one discharge tube 26 is used, the folding mirrors 5 or deflecting mirrors are used to provide increased output power.
- the optical resonator structure 24 is made out of rigid cast aluminum. As a result, the structure 24 is of light weight.
- the end brackets 41 and 43 are kinematically mounted on support member 39.
- the support member 39 is generally parallel with the support tube 40 and with the discharge tubes 26 and the exhaust tube 27.
- the first end bracket 41 is rigidly fastened onto the support member 39.
- a mounting bolt 45 bolts the first end bracket 41 to the structural member 39.
- the bolt 45 is fastened such that it prevents any movement of the end bracket 41 in any direction.
- the second end bracket 43 has a slot 47 therein.
- a slot 47 is located on each side of the second end bracket 43 (only one is shown in FIG. 1).
- a mounting bolt 49 on the structural member 39 is passed through the slot 47.
- the bolts 49 passing through the slot 47 permit the second end bracket 43 to move in directions parallel or perpendicular to the axis of tube 26.
- the bolts 49 prevent the second end bracket 43 from moving in the vertical direction.
- Substantially near the center of the second end bracket 43 is a hole 53 through which an alignment pin 51 passes (as shown in the cut-away section of FIG. 1).
- the alignment pin 51, through the slot 53 prevents the second end bracket 43 from moving in the horizontal direction perpendicular to the axis of tube 26.
- the overall effect of the bolts 49 and the alignment pin 51 is to permit the second end bracket 43 to move only in the direction parallel to the axis of tube 26.
- FIG. 3 shows gas inlet passageways 72 through which gas may flow from the interior of support tube 40 into each gas discharge tube 26.
- Each rod-shaped anode 65 is surrounded by fitting 73, and each fitting 73 is attached to housing 71.
- Fitting 73 provides a seal preventing gas from flowing from passage 72 to the exterior of housing 71.
- One end of anode 65 is positioned adjacent gas inlet orifice 74 in the sidewall of ceramic bushing 101, so as to be in electrical communication with gas flowing through orifice 74 into the interior of ceramic bushing 101 (bushing 101 comprises a portion of tube 26).
- Electrical lines 70 connect each of anodes 65 to an appropriate electric power source.
- each gas inlet passageway 72 supplies gas from tube 40 to tube 26 through two orifices in the sidewall of tube 26. Only one orifice for each tube 26 is shown in the FIG. 3 view of the system, but both orifices are shown in FIG. 4 (which is a variation of the gas inlet means shown in FIG. 3 to be discussed below).
- Anode 65' held by fitting 73', is positioned adjacent the second orifice (not shown in FIG. 3) in the same manner as anode 65 is positioned adjacent the first orifice (orifice 74 of FIG. 3).
- the two orifices are separated from each other by a short distance along the axis of tube 26, so that anode 65' lies below the plane of FIG. 3 (into the page) whereas anode 65 lies in the plane of FIG. 3.
- FIG. 4 is a cross-sectional view, of a preferred embodiment of a gas inlet means that may be used in the inventive system, in a horizontal plane containing the longitudinal axis of tube 26.
- Ceramic bushing 101 is fitted around the end portions of sections 26a and 26c of tube 26, so that ceramic bushing 101 comprises section 26b of tube 26.
- Housing 102 surrounds the middle section of bushing 101, and includes gas inlet passages 106 and 108.
- O-ring seals 104 prevent gas from escaping outside housing 102 from within housing 102. Gas may flow from passage 106, past orifice 118 in the sidewall 122 of ceramic bushing 101, into interior 107 of ceramic bushing 101.
- gas may flow from passage 108, past orifice 120 in sidewall 122 of ceramic bushing 101 into interior 107 of ceramic bushing 101.
- Gas inlet passages 106 and 108 may be portions of a common gas passageway, or may be separate passages.
- Electrodes 110 and 112 are held in position by housing 102 so that their respective end portions 114 and 116 are disposed adjacent orifices 118 and 120, respectively. Electrodes 110 and 112 are thus in electrical communication with gas flowing through the orifices into tube 26. Each electrode is held by fitting 130 (which is preferably of the Cajon Ultratorr type), which fitting is attached to housing 102. Fittings 130 prevent gas from escaping from passages 106 and 108 to the exterior of housing 102.
- Pressurized gas flowing past orifice 118 (and 120) will initially flow against the portion of sidewall 122 opposite the orifice, and will then flow in an eddy current such as that defined by arrows 200 (and 201), before flowing away from the orifice (and from the adjacent orifice) in the directions of arrows 202 (and 203).
- the gas flowing in tube 26 downstream from the orifice pair have a flat velocity profile (i.e., a graph of the gas flow velocity, versus the radial distance away from the sidewall of tube 26, should approximate a straight line with zero slope).
- a flat velocity profile i.e., a graph of the gas flow velocity, versus the radial distance away from the sidewall of tube 26, should approximate a straight line with zero slope.
- the gas velocity profile is much less flat (i.e., spans a much greater range of velocities) than if the orifices are located on opposite sides of sidewall 122 (as shown in FIG. 4) so that the two orifices are separated by an azimuthal angle substantially equal to 180° (so that gas jets entering interior 107 of tube 26 have antiparallel orientation).
- the resulting gas velocity profile will be flatter than if the azimuthal angle were 0° but will generally not be as flat as in the case that the azimuthal angle is 180°.
- the orifices be located with relative azimuthal separation substantially equal to 180° as shown in FIG. 4.
- each electrode should be positioned away from the center of the orifice. That is, where the longitudinal axis of the elongated electrode is positioned substantially perpendicular to the plane of the orifice (as in FIG. 4, where the axis of electrode 110 points toward the bottom of the Figure and the plane of orifice 118 is colinear with sidewall 122), the electrode's longitudinal axis should not coincide with a perpendicular line through the center of the orifice.
- the longitudinal axis of the electrode need not be oriented perpendicular to the plane of the orifice, but the projection of the tip of the electrode on the plane of the orifice should always be spaced away from the center of the orifice. This configuration results in a much flatter gas velocity profile than in the case that the projection of the electrode tip does coincide with the orifice center.
- FIGS. 5 and 6 indicate preferred dimensions and relative position of each electrode-orifice pair in the FIG. 4 system.
- FIG. 5 is a view of the left half of the FIG. 4 apparatus taken along line 5--5 of FIG. 4.
- the orifice is disc-shaped and has diameter substantially equal to half an inch (0.5").
- FIG. 6 is an enlarged mirror-image view of the end portion of electrode 110 and orifice 118. Tip T of electrode 110 is offset upstream from center point C of orifice 118 by a distance in the range from about 0.08" to about 0.10".
- the electrode may be either a cathode or an anode.
- both electrodes should be of the same type (either both anodes or both cathodes).
- the anode of the laser resonator be positioned upstream (in the axial gas flow) with respect to the nearest cathode to enhance the light discharge resulting from application of the electric field to the flowing gas between the anode and cathode.
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- Electromagnetism (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Optics & Photonics (AREA)
- Lasers (AREA)
Abstract
Description
Claims (19)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/101,130 US4799231A (en) | 1987-09-24 | 1987-09-24 | Laser gas orifice injection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/101,130 US4799231A (en) | 1987-09-24 | 1987-09-24 | Laser gas orifice injection system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US4799231A true US4799231A (en) | 1989-01-17 |
Family
ID=22283173
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US07/101,130 Expired - Lifetime US4799231A (en) | 1987-09-24 | 1987-09-24 | Laser gas orifice injection system |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US4799231A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6061375A (en) * | 1996-11-01 | 2000-05-09 | Semiconductor Energy Laboratory, Inc. | Laser irradiation system and application thereof |
| US6580742B1 (en) * | 1999-10-12 | 2003-06-17 | Matsushita Electric Industrial Co., Ltd. | Laser oscillating apparatus |
| US20030139066A1 (en) * | 1996-12-12 | 2003-07-24 | Semiconductor Energy Laboratory Co., Ltd. | Laser annealing method and laser annealing device |
| CN103022871A (en) * | 2011-10-14 | 2013-04-03 | 开天激光有限公司 | Resonance cavity type fast-flow axial laser device system |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4470144A (en) * | 1981-05-18 | 1984-09-04 | Matsushita Electric Industrial Company, Limited | Coaxial-type carbon dioxide gas laser oscillator |
| US4481632A (en) * | 1981-09-12 | 1984-11-06 | Messer Griesheim Gmbh | Laser, particularly CO2 gas transport laser |
| US4502145A (en) * | 1983-05-06 | 1985-02-26 | Coherent, Inc. | Power supply for a laser |
| GB2158635A (en) * | 1983-12-29 | 1985-11-13 | Amada Eng & Service | High-speed axial flow type gas laser oscillator |
| US4622675A (en) * | 1983-07-29 | 1986-11-11 | P.R.C., Ltd. | Forced transport molecular gas laser and method |
| US4635272A (en) * | 1981-11-04 | 1987-01-06 | Kimmon Electric Co., Ltd. | Laser discharge tube |
| US4646310A (en) * | 1986-01-08 | 1987-02-24 | Amada Engineering Service Co., Inc. | Flow control device for a laser generator |
| US4660209A (en) * | 1983-12-29 | 1987-04-21 | Amada Engineering & Service Co., Inc. | High speed axial flow type gas laser oscillator |
| US4661958A (en) * | 1983-05-06 | 1987-04-28 | Coherent, Inc. | Laser |
| US4672621A (en) * | 1982-04-13 | 1987-06-09 | Matsushita Electric Industrial Co., Ltd. | Laser resonator having an improved gas-introducing portion |
| US4701925A (en) * | 1985-07-22 | 1987-10-20 | Koito Seisakusho Co., Ltd. | Electric control system for a metal ion laser |
-
1987
- 1987-09-24 US US07/101,130 patent/US4799231A/en not_active Expired - Lifetime
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4470144A (en) * | 1981-05-18 | 1984-09-04 | Matsushita Electric Industrial Company, Limited | Coaxial-type carbon dioxide gas laser oscillator |
| US4481632A (en) * | 1981-09-12 | 1984-11-06 | Messer Griesheim Gmbh | Laser, particularly CO2 gas transport laser |
| US4635272A (en) * | 1981-11-04 | 1987-01-06 | Kimmon Electric Co., Ltd. | Laser discharge tube |
| US4672621A (en) * | 1982-04-13 | 1987-06-09 | Matsushita Electric Industrial Co., Ltd. | Laser resonator having an improved gas-introducing portion |
| US4502145A (en) * | 1983-05-06 | 1985-02-26 | Coherent, Inc. | Power supply for a laser |
| US4661958A (en) * | 1983-05-06 | 1987-04-28 | Coherent, Inc. | Laser |
| US4622675A (en) * | 1983-07-29 | 1986-11-11 | P.R.C., Ltd. | Forced transport molecular gas laser and method |
| GB2158635A (en) * | 1983-12-29 | 1985-11-13 | Amada Eng & Service | High-speed axial flow type gas laser oscillator |
| US4660209A (en) * | 1983-12-29 | 1987-04-21 | Amada Engineering & Service Co., Inc. | High speed axial flow type gas laser oscillator |
| US4701925A (en) * | 1985-07-22 | 1987-10-20 | Koito Seisakusho Co., Ltd. | Electric control system for a metal ion laser |
| US4646310A (en) * | 1986-01-08 | 1987-02-24 | Amada Engineering Service Co., Inc. | Flow control device for a laser generator |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6061375A (en) * | 1996-11-01 | 2000-05-09 | Semiconductor Energy Laboratory, Inc. | Laser irradiation system and application thereof |
| US20030139066A1 (en) * | 1996-12-12 | 2003-07-24 | Semiconductor Energy Laboratory Co., Ltd. | Laser annealing method and laser annealing device |
| US7351646B2 (en) | 1996-12-12 | 2008-04-01 | Semiconductor Energy Laboratory Co., Ltd. | Laser annealing method and laser annealing device |
| US20080213986A1 (en) * | 1996-12-12 | 2008-09-04 | Semiconductor Energy Laboratory Co., Ltd. | Laser annealing method and laser annealing device |
| US7687380B2 (en) | 1996-12-12 | 2010-03-30 | Semiconductor Energy Laboratory Co., Ltd. | Laser annealing method and laser annealing device |
| US6580742B1 (en) * | 1999-10-12 | 2003-06-17 | Matsushita Electric Industrial Co., Ltd. | Laser oscillating apparatus |
| CN103022871A (en) * | 2011-10-14 | 2013-04-03 | 开天激光有限公司 | Resonance cavity type fast-flow axial laser device system |
| CN103022871B (en) * | 2011-10-14 | 2015-04-29 | 开天激光有限公司 | Resonance cavity type fast-flow axial laser device system |
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